A calculator program for analyzing airloads on a wing of arbitrary planform and camber in subsonic flow

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049 ‡aMAIN
086 0 ‡aD 301.45/46-2:77-136
100 1 ‡aSparks, John C., ‡eauthor.
245 1 2 ‡aA calculator program for analyzing airloads on a wing of arbitrary planform and camber in subsonic flow / ‡cJohn C. Sparks.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, ‡c1978.
300 ‡avi, 48 pages: ‡billustrations ; ‡c28 cm
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 77-136
500 ‡a"Final report for period 1 April 1976 to 31 August 1976."
500 ‡a"January 1978."
504 ‡aIncludes bibligraphic references (page 48)
520 ‡aA subsonic airloads program for small (8-K) calculators is presented. Features include good man-machine interaction and quick turn-around which speed preliminary design. The program is written in BASIC for the HP9830 or HP9831 calculator systems equipped with Matrix ROM and 9862A plotter. Programming techniques illustrated may be applied to any small system having special function keys or an equivalent capability. (Author).
538 ‡aMode of access: Internet.
650 0 ‡aCamber (Aerofoils)
650 0 ‡aAerofoils ‡xComputer programs.
650 0 ‡aAerodynamic load ‡xMeasurement ‡xComputer programs.
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095319052
CID ‡a102856107
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